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Add Chimera combined-cycle ramjet (#2988)
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GameData/RealismOverhaul/Engine_Configs/Jet_Engine_Configs/Chimera_Config.cfg
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// ================================================== | ||
// Engine: Chimera | ||
// | ||
// Manufacturer: Hermeus & GE | ||
// | ||
// ================================================================================= | ||
// J85-GE-21 | ||
// 1972, F-5E/F | ||
// Engine core consists of J85s from retired F-5Es | ||
// | ||
// Dry Mass: 480 kg //guess, ramjet+precooler | ||
// Thrust (Dry): 16.0 kN | ||
// Thrust (Wet): 24.4 kN //afterburner replaced with combined cycle ramjet. More thrust augmentation than stock afterburner? | ||
// SFC (Dry): 1.24 lb/lbf-hr | ||
// Area: 0.085 m^2 //Compressor Area | ||
// BPR: 0.0 //Bypass Ratio | ||
// CPR: 8.1 //Compressor Pressure Ratio | ||
// FPR: 0.0 //Fan Ratio | ||
// Mdes: 0.9 M //Mach Design Point | ||
// Tdes: 250 K //Temp Design Point | ||
// eta_n: 0.9 //Efficiency at afterburner rear / nozzle entrance | ||
// FHV: 28000000 J //Fuel heat of burning | ||
// TIT: 1300 K //Combustion peak temp | ||
// TAB: 1927* K //Afterburner peak temp | ||
// maxT3: 865 K //Turbine max temperature some precooling to push J85 core to M3 | ||
// Exhaust Mixer: false | ||
// Adjustable Nozzle: true | ||
// ================================================================================= | ||
// Chimera | ||
// 2022 | ||
// Envelope M3 to M5 (@ altitude?). Mostly copied from XRJ59 | ||
// | ||
// Dry Mass: N/A kg | ||
// Thrust: 36.6 kN //guess | ||
// Area: 0.125 m^2 //Compressor Area | ||
// Mdes: 4.0 M //Mach Design Point | ||
// Tdes: 225 K //Temp Design Point | ||
// eta_n: 0.98 //Efficiency at afterburner rear / nozzle entrance | ||
// FHV: 32400000 J //Fuel heat of burning | ||
// maxFar: 0.07 //Max fuel to air ratio | ||
// maxEngineTemp: 4370 K //Engine max temperature | ||
// ================================================================================= | ||
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// Sources: | ||
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// https://www.hermeus.com/chimera | ||
// https://www.hermeus.com/press-release-tbcc-milestone | ||
// https://www.jet-engine.net/miltfspec.htm | ||
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// Used by: | ||
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// Notes: | ||
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// Run on test stand, but never flown? Quarterhorse demonstrators appear to use normal J85s, with | ||
// F100-based design intended for full-scale model. | ||
// ================================================== | ||
@PART[*]:HAS[#engineType[Chimera]]:FOR[RealismOverhaulEngines] | ||
{ | ||
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%title = #roChimeraTitle //Chimera Combined Cycle Ramjet | ||
%manufacturer = #roMfrHermeus | ||
%description = #roChimeraDesc | ||
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@tags ^= :$: usa hermeus ge general electric j85 chimera ramjet turbojet | ||
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%specLevel = prototype //operational, prototype, concept, speculative, altHist, sciFi | ||
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!MODULE[ModuleEngines*],*{} | ||
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MODULE | ||
{ | ||
name = ModuleEnginesAJEJet | ||
EngineType = Turbine | ||
thrustVectorTransformName = thrustTransform | ||
engineID = MainEngine | ||
} | ||
MODULE | ||
{ | ||
name = ModuleEnginesAJERamjet | ||
EngineType = Turbine | ||
thrustVectorTransformName = thrustTransform | ||
engineID = BackupEngine | ||
} | ||
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@MODULE[ModuleAlternator] | ||
{ | ||
@RESOURCE[ElectricCharge] | ||
{ | ||
%rate = 50.0 | ||
} | ||
} | ||
!MODULE[ModuleGimbal]{} | ||
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MODULE | ||
{ | ||
name = ModuleEngineConfigs | ||
type = ModuleEnginesAJEJet | ||
configuration = J85-GE-21-Chimera | ||
engineID = MainEngine | ||
isMaster = True | ||
origMass = 0.480 | ||
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CONFIG | ||
{ | ||
name = J85-GE-21-Chimera | ||
description = Temperature Mach limit at 15 km: 3.16. | ||
specLevel = prototype | ||
massMult = 1.00 | ||
heatProduction = 10 | ||
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Area = 0.085 //Compressor Area | ||
BPR = 0.0 //Bypass Ratio | ||
CPR = 8.1 //Compressor Pressure Ratio | ||
FPR = 0.0 //Fan Ratio | ||
Mdes = 0.9 //Mach Design Point | ||
Tdes = 250 //Temp Design Point | ||
eta_c = 0.95 //Efficiency at burner inlet | ||
eta_t = 0.98 //Efficiency at burner exit | ||
eta_n = 0.9 //Efficiency at afterburner rear / nozzle entrance | ||
FHV = 28000000 //Fuel heat of burning (joules?) | ||
TIT = 1300 //Combustion peak temp | ||
TAB = 2498 //Afterburner temp? | ||
maxT3 = 865 //Turbine max temperature | ||
exhaustMixer = False | ||
adjustableNozzle = True | ||
thrustUpperLimit = 50 | ||
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// Engine fitting params | ||
defaultTPR = 0.85 | ||
dryThrust = 16 | ||
wetThrust = 24.4 | ||
maxThrust = 24.4 //Just to let MEC know thrust | ||
drySFC = 1.24 | ||
throttleResponseMultiplier = 0.6 //70s single-spool, 0.6 | ||
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PROPELLANT | ||
{ | ||
name = Kerosene | ||
ratio = 1.0 | ||
DrawGauge = True | ||
} | ||
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OtherModules | ||
{ | ||
BackupEngine = Chimera | ||
} | ||
} | ||
} | ||
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MODULE | ||
{ | ||
name = ModuleEngineConfigs | ||
type = ModuleEnginesAJERamjet | ||
configuration = Chimera | ||
engineID = BackupEngine | ||
isMaster = False | ||
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CONFIG | ||
{ | ||
name = Chimera | ||
//description = | ||
specLevel = prototype | ||
massMult = 1.00 | ||
heatProduction = 10 | ||
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Area = 0.125 //Compressor Area | ||
Mdes = 4.00 //Mach Design Point | ||
Tdes = 225 //Temp Design Point | ||
eta_n = 0.98 //Efficiency at afterburner rear / nozzle entrance | ||
FHV = 32400000 //Fuel heat of burning (joules?) | ||
maxFar = 0.10 | ||
maxEngineTemp = 4370 | ||
thrustUpperLimit = 45 | ||
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// Engine fitting params | ||
maxThrust = 45 //Just to let MEC know thrust | ||
throttleResponseMultiplier = 1.0 | ||
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PROPELLANT | ||
{ | ||
name = Kerosene | ||
ratio = 1.0 | ||
DrawGauge = True | ||
} | ||
} | ||
} | ||
} |
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